Coriolis flow sensor

ABSTRACT

A Coriolis flow sensor including a loop-shaped Coriolis tube mounted in a housing with two ends lying next to one another, the ends being fixed in a fixation element, while the portion of the tube located between the ends lies free from the housing, which flow sensor includes an excitation element for causing the tube to oscillate about an excitation axis as well as a detection element for detecting displacements of portions of the tube during operation. The tube is connected through the fixation element to a balancing member, the assembly of the balancing member and the tube being resiliently arranged with respect to the housing, while the excitation element are arranged to rotate the tube and the balancing member with counter-phase about the excitation axis

The invention relates to a Coriolis flow sensor comprising a loop-shapedCoriolis tube mounted in a housing with two ends lying next to oneanother, said ends being fixed in a tube fixation means, while theportion of the tube located between said ends lies free from thehousing, which flow sensor comprises excitation means for causing thetube to oscillate about an excitation axis as well as detection meansfor detecting displacements of portions of the tube during operation.

Such a flow sensor having a loop-shaped Coriolis tube is known from EP 1719 982 A1. Various types of loop-shaped Coriolis tubes are describedtherein, both of the single loop type and of the (continuous) doubleloop type. The present invention relates to any of these types, but isnot restricted thereto.

A Coriolis flow sensor (or Coriolis flow sensor system) comprises atleast one vibrating tube, often denoted Coriolis tube, flow tube, orsensing tube. This tube or these tubes is or are fastened at both endsto the housing of the instrument. These tube ends serve at the same timeas feed and discharge ducts for the liquid or gas flow to be measured.

Besides the flow tube (or tubes), a Coriolis flow sensor comprises twofurther subsystems, i.e. one for excitation and one for detection. Theexcitation system (exciter) brings the tube into vibration. For thispurpose, one or several forces or torques are applied to portions of thetube. The detection system usually detects the displacements of one orseveral points of the tube as a function of time. Instead of thisdisplacement, the force (or torque) exerted by the tube on itsenvironment may alternatively be measured; what will be described belowwith reference to displacement detection is equally valid for forcedetection.

The same two placement alternatives are possible for excitation anddetection. One is to have the excitation and detection take placebetween the housing and the tube. The other one is to have theexcitation or detection take place between different points or sectionsof the moving flow tube or—if the instrument has several tubes—betweenthe individual tubes.

In the case of a Coriolis flow sensor (also referred to as “the (sensor)instrument” or “the flowmeter” hereinafter) designed for measuring smallflows, it is desirable for the entire tube to lie in one plane both forthe purpose of the measuring accuracy and for the purpose of ease ofmanufacture.

The vibration of the tube generated by the exciter takes place at a moreor less fixed frequency which varies slightly only as a function of thedensity of the medium flowing through the tube. The vibration frequencyis almost always a natural frequency of the tube so that a maximumamplitude can be achieved with a minimum energy input.

The invention is based on the recognition that two vibration problemsmay arise as a result of the vibration of the tube if no additionalmeasures are taken.

The first problem may arise when two identical instruments are locatedclose to one another while their vibration frequencies substantiallycoincide. One instrument may then excite the other instrument via thehousing and the supporting surface, in general just outside its naturalfrequency, with a phase that will practically always differ from that ofits own excitation. This is a real problem, because in practice, forexample in mixing processes, two, three, or sometimes up to twentyflowmeters are arranged next to one another. It is found then that themeasuring results can vary with a certain periodicity independently ofthe flow.

A second problem is the sensitivity to own vibrations: when a Coriolisflowmeter is placed on a non-rigid surface, for example a thin plate, orin a system of ducts, said surface may start to vibrate along with theflowmeter. The own vibrations are seen as shifts in the zero point. Theaccuracy of the sensor, and thus of the measurement, is influencedthereby in an unpredictable manner.

It is an object of the invention to reduce the sensitivity to vibrationsof a Coriolis flow sensor, especially of Coriolis flow sensors of thetype wherein detection (and excitation) take place with respect to thehousing. It is a particular object to reduce the sensitivity of thesensor instrument to its own vibrations or to vibrations of adjoiningflow sensor instruments.

This object is achieved in a Coriolis flow sensor of the kind describedin the opening paragraph in that the tube through the tube fixationmeans is connected to a balancing member, in that the assembly of thebalancing member and the tube is resiliently arranged with respect tothe housing, and in that the excitation means are arranged for rotatingthe tube about the excitation axis in counter-phase with the balancingmember.

Measurements have shown inter alia that the resilient mounting of theCoriolis tube as described herein reduces the transfer of vibrationsfrom a Coriolis tube to the housing during operation, and that a firstinstrument provided with this resilient mounting interferes with asecond instrument located in the vicinity thereof to a lesser extent. Atthe same time there is a reduced sensitivity to external vibrations,which accordingly leads to an improved accuracy of a lone flow sensorwith a resiliently mounted Coriolis tube. Should external means be usedfor the excitation, however, for example Lorentz excitation means asdescribed in EP 1 719 982 A1, where an alternating current is passedthrough the tube and the tube is placed in the field of an externalpermanent magnet yoke that is fastened to the housing, then it is stillpossible for forces to be exerted on the housing via the magnet yokeduring operation.

This is prevented according to the invention in that the excitationmeans are “internal” and are connected, directly, or indirectly, to thetube fixation means, but are not connected to the housing.

In a preferred embodiment, the tube fixation means is characterized inthat it is of a bipartite construction comprising a first and a secondfixation sub-means, said first fixation sub-means being connected to thebalancing member while the tube ends are fixed in said second fixationsub-means, which fixation sub-means are moveably interconnected, and theexcitation means are designed for causing the second fixation sub-meansto pivot relative to the first fixation sub-means about the excitationaxis.

In particular, the two parts are moveable (pivotable) relative to oneanother through actuation of a first and a second piezoelectric actuatorarranged between the parts. In a preferred embodiment, the first and thesecond piezoelectric actuator are connected to a trigger device so as tobe controlled by respective sinusoidal signals in counter-phase.

In a further embodiment, the assembly of the balancing member and thetube is suspended relative to the housing by resilient means such thatit can rotate about an axis of rotation that is at least substantiallyparallel to or coincides with the excitation axis of the tube.

In a further preferred embodiment, the tube ends merge into a feed tubeand a discharge tube beyond the tube fixation means, which feed tube anddischarge tube are fixedly connected to a feed block and a dischargeblock, respectively, said feed and discharge blocks constituting thesole resilient means. This construction is possible if the tube iscomparatively thick. If the tube is comparatively thin, however, apreferred embodiment is characterized in that the resilient means areformed by an elastic hinge formed from plate material which connectseither the balancing member or the tube fixation means to the housing.

Preferably, the natural frequency of the balancing member (and of theCoriolis tube) is substantially lower than the excitation frequency.This leads to an even better vibration insulation (vibrations aretransmitted with attenuation). To realize this, it is advantageous ifthe balancing member has a mass inertia relative to said axis ofrotation that is substantially greater (in particular a number of timesgreater) than that of the Coriolis tube.

The detection of tube displacements may take place between the tube andthe housing or between different parts of the tube. The principle of theinvention, however, is particularly suitable for application incombination with a detection of displacements of the tube within the‘resilient environment’, i.e. between the tube and the tube fixationmeans. This also reduces the sensitivity to external vibrations. Apreferred embodiment of the invention is for this purpose characterizedin that the detection means comprise at least two optical detectorswhich are arranged next to one another on one of the two constituentparts of the fixation means adjacent to a portion of the tube.

The invention further provides an embodiment which is characterized inthat it comprises an actuator block which has two mutually resilientlyarranged portions between which a single actuator is arranged to movethe portions relative to one another, the first one of these portionsbeing connected to the balancing member, and the second one beingconnected to the tube fixation member.

The use of a single actuator serves to avoid a difference in actuationforce that may occur with two actuators, so that no undesirabledisturbances will occur in the tube movements that could be mistaken fortube movements caused by media flowing through the tube.

A few embodiments of the invention will now be described in more detailwith reference to the drawings. Identical parts have been given the samereference numerals in the Figures.

FIG. 1 is a diagram of a first embodiment of a Coriolis flow sensor witha Coriolis tube according to the invention;

FIG. 2 diagrammatically shows a second embodiment of a Coriolis flowsensor with a Coriolis tube according to the invention;

FIG. 3 diagrammatically shows a third embodiment of a Coriolis flowsensor with a Coriolis tube according to the invention;

FIG. 4 diagrammatically shows a fourth embodiment of a Coriolis flowsensor with a Coriolis tube according to the invention;

FIG. 5 shows the fastening of the Coriolis tube and its twopiezoelectric actuators of FIG. 1 in detail;

FIG. 6 and FIG. 7 are detailed views of alternative fastening methodsfor Coriolis tubes with two piezoelectric actuators according to theinvention;

FIG. 8 shows the Coriolis tube of a Coriolis flow sensor according tothe invention in plan view and in cross-section;

FIG. 9 shows piezoelectric actuators used in FIG. 5 and FIG. 6 inelevation;

FIG. 10 shows a circuit for triggering the actuators of FIG. 9;

FIG. 11 shows a resilient element of the type used in the Coriolis flowsensors of FIGS. 3 and 4;

FIG. 12 shows a Coriolis flow tube with a balancing member having anadjustable mass inertia;

FIGS. 13, 14 and 16 diagrammatically show different elevations of anembodiment of a Coriolis flowsensor with a Coriolis tube with singlepiëzo actuation; and

FIG. 15 shows a perspective view of a part of the flowsensor of FIGS.13, 14, 16, said part surrounding the tube.

FIG. 1 shows an embodiment of a flow sensor 1 of the Coriolis type witha loop-shaped Coriolis (or sensing) tube 2 bent into a rectangle whichfollows a substantially closed path (forms a substantially full turn).The loop-shaped flow (or sensing) tube 2 in this embodiment comprisestwo parallel lateral tube portions 2 a, 2 b which at one end areconnected to a first transverse tube portion 2 e and at the other end totwo second tube portions 2 c, 2 d. The latter are connected to a feedtube portion 2 f and to a discharge tube portion 2 g, respectively, atthe area where they come together, said portions 2 f and 2 g lying closetogether on either side of and symmetrically with respect to the mainaxis of symmetry of the tube 2. The loop 2 and the feed and dischargetube portions 2 f, 2 g preferably form part of one and the same tube.The tube portions 2 f and 2 g form part of a feed tube 3 and a dischargetube 4, respectively. The feed tube 3 is connected to an inlet 6 and thedischarge tube 4 to an outlet 7 via a feed and discharge block 5 whichis connected to the housing or forms part thereof. The feed anddischarge tube portions 2 f, 2 g in this embodiment extend within theloop 2 and are fastened to a fixation block 13 of a tube fixation meansthat comprises two fixation blocks 12 and 13. The fixation block 12 isconnected to a balancing member 8 via an intermediate piece 11. Saidmember 8 comprises a bridge piece 9 which is provided with end weights10 a and 10 b at its extremities. Depending on the envisaged effect, theintermediate piece is rigid (for example comparatively thick) orflexible (for example comparatively thin). The loop 2, the feed anddischarge tube portions 2 f, 2 g, and the feed and discharge tubes 3, 4may advantageously be manufactured from one piece of tubing. This maybe, for example, a stainless steel tube with an external diameter ofapproximately 0.7 mm and a wall thickness of approximately 0.1 mm.

The invention is not only suitable for smaller tube dimensions, forexample external diameter below 1 to 1.5 mm, but also for tubes oflarger diameter, for example 10 mm.

An essential aspect of the invention is that the assembly of theCoriolis tube and the balancing member is resiliently mounted relativeto the housing. The object of this is to make any forces exerted on thehousing when the tube is being excited as weak as possible. Thisresilience is realized in the construction of FIG. 1 in that the feedand discharge tubes 3 and 4 are constructed such that they themselvesprovide the desired resilient behavior. To achieve this, the tubes arecomparatively thick. The construction of FIG. 1 comprises no connectionsbetween the tube 2 and the housing other than the base portions of thefeed and discharge tubes 3 and 4.

If an external excitation were used, however, for example Lorentzexcitation as in EP 1 719 982 A1, where an alternating current is passedthrough the tube and the tube is placed in the field of an externalpermanent magnet yoke that is fastened to the housing, then it is stillpossible for forces to be exerted on the housing via the magnet yokeduring operation. This is prevented according to the invention in thatthe excitation means are provided internally, e.g. exclusively directlyor indirectly at the tube fixation means. According to a firstembodiment the tube fixation block for this purpose comprises two parts12, 13 between which piezoelectric actuators 16, 17 (also denoted piezoshereinafter) are fastened. The piezos 16, 17 are clamped between the twoparts 12, 13 of the fixation block by means of a bolt fastening 14, 15.Resilient means are present below each bolt head, for example in theform of one or more cup springs 28, 29 which apply a defined biastension to the clamping construction of the piezos 16, 17. All this isshown in detail in FIG. 5. Said bias tension can be adjusted in that thebolts 14, 15 are turned back a certain degree from the point at whichthe cup springs are depressed to the maximum (fully flat). As a result,the released bolt length will allow a certain stroke of the cup spring.The combination of the cup spring's stiffness and the stroke thereofprovides the clamping of the piezos 16, 17 with the desired biastension.

The fixation block thus has two parts 12, 13 of which one part 12 isformed, for example, by a milled part (which may alternatively beobtained in a casting process). This is a milled or die-cast product inwhich the bridge piece 9 together with the additional end weights 10 a,10 b fastened thereto forms the balancing member 8. An intermediatepiece 11 of this milled part is so narrow that it is flexible in atorsion direction at a certain frequency. During normal operation (atthe oscillation frequency of the tube) and given such a narrowintermediate piece 11, the balancing member 8 and the loop of theCoriolis tube, i.e. portions 2 a to 2 e, will thus start moving incounter-phase such that the first and the second tube fixation means 12,13 are substantially stationary in the optimum situation. Theintermediate piece 11 and the tube portions 2 f, 2 g act as theresilient elements herein. In the case of a rigid intermediate piece 11,the entire assembly of the parts 8, 11, 12, 13 will move incounter-phase with the loop of the Coriolis tube, i.e. portions 2 a to 2e, during which only the tube portions 2 f, 2 g act as the resilientelements. The sensor tube 2 is fastened in a recess, for example bymeans of a brazing process, at the other end 13 of the tube fixationmeans.

As is visible in FIGS. 9 and 10, the piezos 16, 17 are provided withconnection wires. The piezos will expand or shrink in the direction ofthe clamping under the influence of a positive or negative voltage. Whena sinusoidal AC voltage is applied (FIG. 10), the piezos will followthis signal by shrinking and expanding. The piezos are connectedelectrically in parallel but in counter-phase. As a result, the onepiezo will expand at a given voltage and the other one will shrink tothe same extent. The piezos each generate a force that runs counter tothe bias tension of the relevant cup spring and that accordingly leadsto a net displacement. Upon a shrinkage at the other side, the cupspring will compress the assembly further. The application of asinusoidal signal to the piezos in counter-phase will cause the piezosand the construction together to perform a reciprocating torsional, i.e.pivoting movement.

The tube vibrations are measured by optical sensors. Additionalelectronics and firmware process and amplify the measured signals sothat the Coriolis sensing tube 2 oscillates at its natural frequency. Atypical voltage for the piezos is approximately 30 V. Since the tubeoscillates at its natural frequency with a high Q (quality) factor ofapproximately 2000, the piezos account for no more than 1/Q of theamplitude. The rest of the amplitude is caused by the physicalphenomenon of resonance.

The excitation means for causing the loop-shaped tube 2 to oscillateabout its main axis of symmetry (also denoted primary or excitation axisof rotation) comprise two piezoelectric actuators 16, 17 in theconstruction of FIG. 1. As is shown in FIG. 9, the actuators 16, 17 areannular bodies. The threaded bolts 14, 15, which are located on eitherside of the tube portions 2 f and 2 g and are symmetrical thereto, arepassed through the openings in these annular bodies. As FIG. 6 shows foran alternative embodiment, the piezo actuators 26, 27 may be rectangularplates. These will then be arranged at the outer side of the bolts 24,25 which together with (cup) springs 28′, 29′ exert a clamping force onthe fixation sub-blocks 22, 23. FIG. 1 further shows a system of (three)optical sensors 20 which is fastened to a plate 18 that is fastened tothe feed and discharge block 5, i.e. to the fixed outer world. Thissystem of optical sensors corresponds to the system disclosed in EP 1719 982 A1 which forms part of the present description by reference.

FIG. 2 shows a more favorable embodiment, also of the so-termedbox-in-a-box type, i.e. also spring-loaded exclusively via comparativelythick feed and discharge tubes 3, 4, but in this case with the system ofthe (three) optical sensors 20 at (a projection of) the tube fixationblock 12 (the fixation sub-means that is connected to the balancingmember 8 or forms part thereof). The system is located in the vicinityof tube portion 2 e of the Coriolis sensing tube 2 with two opticalsensors lying next to one another symmetrically relative to theexcitation axis. The third optical sensor may serve for correctionpurposes. It is, however, also practicable to fasten the system ofoptical sensors 20 to the tube fixation block 13 (the fixation sub-meansto which the Coriolis tube is attached). This is because the relativemovement between the first and the second fixation sub-means is muchsmaller than the movements of the tube owing to the resonance of thetube.

FIG. 3 shows a flow sensor embodiment according to the invention whereinthe assembly of the Coriolis tube 2 and the balancing member 8 arespring-loaded by a resilient means 21 fastened to the balancing member8. This resilient means 21 (also denoted roof spring on account of itsshape) will be described with reference to FIG. 11. The system 20 of(three) optical sensors is fixed to the tube fixation means, not to thehousing. The optical sensors may be fastened to the housing (as in theconstruction of FIG. 1), if so desired, which is constructionallyeasier, but less appropriate in principle.

FIG. 4 shows a flow sensor arrangement according to the inventionwherein the resilience of the assembly of the Coriolis tube 2 and thebalancing member 8 is obtained via a spring means 21′ fastened to thetube fixation means. This construction has a better vibration-insulatingeffect than that of FIG. 3. Two discs of piezoelectric material 16, 17(annular in shape in this case) are inserted between the tube fixationblock 13, to which the Coriolis tube 2′ is fastened, and the end of thetail piece of the balancing member 8. Also shown is a system 20 of(three) optical sensors (U-shaped blocks) fastened to that same end ofthe tail piece. Connection wires of the piezos 16, 17 have not beenshown as they would have rendered the Figure less clear.

FIG. 5 shows in detail the embodiment of FIGS. 1, 2, 3, and 4 of afixation means 12, 13 with piezo excitation by two annular piezos 16, 17arranged around fastening bolts 14, 15. Only the lateral sides of thetwo piezo rings 16, 17 are visible in the Figure.

FIG. 6 shows in detail an embodiment with piezo excitation by tworectangular piezos 26, 27 arranged outside the fastening bolts. Only thelateral sides of the two piezo ‘tiles’ are visible in the Figure.

FIG. 7 shows in detail an embodiment with annular piezos 32, 33, whichpiezos are not in one plane but are mounted obliquely. This may also beconstructed with rectangular piezos.

FIG. 8 shows an embodiment similar to that of FIG. 5, but here thethreaded joint by means of which the bias tension springs for the piezoscan be adjusted is fully visible. In the cross-sectional view takenthrough the center of the tube fixation means, two stacks 28′, 29′ ofcup springs are clearly visible (in fact, twice two cup springs placedone inverted on top of the other), held between the bolt heads 24 and 25and the fixation block 23. The cross-sectional view also shows twopiezos 26, 27 located outside the bolts 24, 25 in recesses of thefixation block 23 as well as the fixation block 22 which forms as itwere the end of the tail piece of the balancing member. The fixationblock 22 in this case is provided with bores having an internal thread34, 35 into which the threaded bolts 24, 25 can be screwed. In analternative embodiment, the bolts are screwed in from below and the cupsprings are also present there. In a mixed version, the bores in thefixation block do not have a screw-thread, but bolts with threaded endsare used onto which nuts can be turned on top of the cup springs.

FIG. 9 shows on an enlarged scale two different shapes for piezoactuators: rectangular (26, 27) and annular (16, 17). The rectangularones are more suitable for use in small sensors, the annular ones foruse in larger sensors.

FIG. 10 is a diagram showing the connection of the piezo actuators 26,27. A device 35 provides a phase locked loop algorithm from whichsetpoints for the frequency and the amplitude of the output signal arederived. The output signal is amplified in an amplifier 36. The latterprovides two signals in counter-phase with which the actuators 26 and 27are controlled.

The embodiment of the resilient means 21, 21′ shown in FIGS. 3 and 4 isa so-termed folded elastic hinge: a flanged resilient plate withintegrated abutments. In this embodiment, two torsion spring elementsand abutments in all three orthogonal directions have been combined intoa single component: a flanged metal plate of resilient material. This isshown more clearly in FIG. 11.

FIG. 11 shows a resilient means 21, 21′ in the form of a rectangularplate of resilient material, such as spring steel, from which a fixedportion 81 (base plate) and within the latter a movable portion 82(carrier plate) are formed in that two incisions are made, whichincisions extend partly longitudinally and partly transversely theretoand are symmetrical relative to the longitudinal axis. The plate is bentalong a folding line 87 and the lateral portions 88, 88′ are folded backso as to lie in one plane in this case. The pairs of mutually facingincisions define resilient bridges 83, 83′ which interconnect the fixedand the movable portion adjacent the ends of the folding line 87.Alternative constructions may have lateral edges which do not lie in oneplane or lateral edges which have not been folded back. The base platemay also be folded along two lines instead of one, such that a planarsurface is present between the flanged sides. The base plate is fastenedto the housing, for example by its lateral edges. The incisionsdelimiting each bridge each account for approximately half the edge of ahole. What remains serves as an abutment. The holes may be, for example,round, oval or elongate. Two of these holes form an elastic hinge withintegrated abutments. Furthermore, it is a folded hinge, wherein thefold achieves that the construction is rigid in two translationdirections (located in a plane transverse to the folding line 87 thatdefines the axis of rotation) instead of one, and the integratedabutments are also active in these two translation directions. The axisof rotation of the construction thus formed lies approximately in thetip of the folding line 87 of the plate. The slits 89 formed by theincisions (four in number) define the maximum possible movementamplitude between the fixed and the moving portion. The relativemovement is greatest at the points 86: an abutment is created in twodirections for each of the four points 86 in that the path of therelevant incision is made to curve back here. Holes 84 arranged in thelateral edges 88, 88′ serve for fastening the fixed portion 81 in thehousing of a flow sensor by means of bolts. An alternative fasteninginstead of bolts is, for example, spot welding. A balancing member isfastened to the movable portion in the points 85, the crossesrepresenting spot welds here. The metal plate with the incisions thereinas shown may be manufactured by laser cutting or etching andsubsequently be folded in an angle bending machine or some other bendingtool.

FIG. 12 shows a Coriolis tube 2 that is resiliently positioned on a feedand discharge block 5. The tube 2 is fastened to a fixation block 12which is connected via a fixation block 13 and an intermediate piece 11to a balancing member 38. The balancing member comprises a connecting orbridge piece 39 which is provided with end weights 40 a and 40 b at itsextremities. The natural frequency of the tube 2 varies with the densityof the medium. The inventors have recognized that the resilient elementsof the balancing member and of the tube should be mutually attuned suchthat the natural frequencies are equal as much as possible relative tothe tube fixation element. This is desirable for generating minimumvibrations towards the housing for all possible densities of the mediumin the tube. It is possible to adapt the natural frequency of thebalancing member 38 in that either the mass inertia thereof is adjustedor the rigidity with which the balancing member is fastened to itssurroundings.

FIG. 12 shows an embodiment of the adaptation of the mass inertia bymeans of an adjustment tool; in this case an adjustment motor 41 that isconnected to two threaded spindles. When the motor 41 is energized, thetwo ends weights 40 a, 40 b can be shifted symmetrically relative to thecenterline H of the bridge piece 39. Two parallel blade springs 42 a, 42b and 43 a, 43 b are shown for each side, which springs provide supportin the one degree of freedom as well as guiding in the other degrees offreedom. This guiding, however, may also be provided in an alternativemanner such as by ball or plain bearings. An alternative is that it isnot the mass inertia that is adapted, but the rigidity with which thebalancing member is fastened to its surroundings. This is the sum of therigidity of the intermediate piece 11 and that of the resilient means inthe case in which the assembly of the tube 2 and the balancing member issuspended from the housing by means of a resilient means (roof spring)fastened to the balancing member (cf. FIG. 3).

A method of providing the desired adjustment in this case compriseschanging the geometry of the lever of a resilient element of theconstruction (the intermediate piece or the roof spring) by means of anadjustment motor. The adjustment possibilities described above alsorequire a control mechanism (not shown). Various embodiments thereof areconceivable. The simplest one is to measure the movements (with amovement sensor at the tube fixation block, or with the optical sensors)and to adjust them to zero. An alternative is to use the naturalfrequency known from the processing together with a previouslydetermined relation so as to perform a correction.

FIG. 13 diagrammatically shows a flow sensor embodiment with a Coriolistube 46 in front elevation. The tube 46 in this case has the shape of acontinuous double loop with an inlet end and an outlet end and ischaracterized by the so-termed box-in-a-box principle. This means thatthe suspension and resilience of the Coriolis tube 46 are realizedexclusively by means of the comparatively thick feed and dischargetubes, 44 and 45 in this case, as in the embodiment of FIGS. 1 and 2,while the displacement of the Coriolis tube 46 and the tube fixationblock 47 takes place relative to a balancing member 48. The balancingmember 48 is of the type shown in the preceding embodiments, i.e. itcomprises a bridge piece with a weight at either end. In the presentcase, the bridge piece consists of two plate parts of which one is shownin FIG. 13. The relevant displacement is imposed by a single piezoactuator 49 which causes the mutually resiliently arranged portions 50a, 50 b of the actuator block 50 (shown in more detail in FIG. 15) tomove relative to one another in the construction of FIG. 13. Theactuation direction of the actuator is chosen to be perpendicular to thepossible directions of movement of the tube. The use of a singleactuator 49 serves to avoid a difference in actuation force that mayoccur with two actuators, so that no undesirable disturbances will occurin the tube movements that could be mistaken for tube movements causedby media flowing through the tube. The tube 46 has two parallel tubeportions, i.e. the outer tubes, and two central vertical tube portions,i.e. the middle tubes, interconnected by respective transverse tubes.

The deformation of the piezoelectric element of the piezo actuator 49will cause the portions 50 a, 50 b of the actuator block 50 to moverelative to one another (however, an alternative actuation principleachieving the same effect may be used instead of this piezoelectricdrive, for example an electro-mechanic principle). Block portion 50 a isconnected to the balancing mass 48 and block portion 50 b to the twocentral vertical portions (the middle tubes) of the Coriolis tube 46 viathe tube fixation block 47. Since the actuator block portions 50 a, 50 bare interconnected by an elastic hinge (50 c in FIG. 15), the tube willstart rotating about its excitation axis X in counter-phase with thebalancing member 48 under the influence of the applied actuation. Theobject of this is, which is essential for the operation of theinstrument, that the entire assembly of actuator block and fixationblock during actuation is stationary with respect to the material worldoutside the instrument. FIG. 13 further shows a frame 51 by means ofwhich sensors are connected to the actuator block portion 50 b such thatdeformations of the tube caused by a medium flowing through the tube canbe detected. (Compare the construction of FIG. 2) The entire assembly isconnected to a connection block 52 via the feed and discharge tubes 44,45.

FIG. 14 is a perspective rear view of the flow sensor of FIG. 13. It isvisible herein how the two portions 50 a, 50 b of the actuator block 50are flexibly interconnected by means of a recessed hinge 50 c. Theportion 50 a of the actuator block 50 is fastened to a tube fixationblock 47 which in its turn is fixed to the two central vertical portions(middle tubes) of the tube 46. The other portion 50 b of the actuatorblock 50 is connected to the balancing mass 48. When the two portions 50a and 50 b move, the tube 46 and the balancing mass 48 will rotate incounter-phase relative to one another about a common point.

FIG. 15 is a more detailed view of the actuator block 50 as used in theembodiment of FIGS. 13 and 14 for causing the tube and the balancingmember to rotate in counter-phase relative to one another. It isapparent how the two actuator block portions 50 a and 50 b areinterconnected via the recessed elastic hinge 50 c, with the piezoelement 49 arranged between the ends of these actuator block portions. Afiller block 53 serves to fill up the space between the actuator blockportions 50 a, 50 b and the piezo 49. Preferably, a tensioning devicemay be provided in both legs of the actuator block portions 50 a, 50 badjacent the piezo 49, for performing in principle the same function asthe bias tensioning device in the embodiment with a double piezo asshown in FIG. 6, a such tensioning device extending parallel to theactuation direction of the piezo 49. A sensor support frame 51 ispresent which is connected to the actuator block portion 50 b.

FIG. 16 is a perspective view of the lower side of the flow sensorassembly of FIGS. 13 and 14. It is visible herein how the actuator blockportion 50 a of the actuator block 50 is connected to the tube fixationblock 47, the latter being fastened to the central vertical portions(middle tubes) of the tube 46.

Summarizing, the invention relates to a Coriolis flow sensor comprisinga Coriolis tube mounted in a housing with two ends lying next to oneanother, said ends being fixed in a fixation means, while the portion ofthe tube located between said ends lies free from the housing, whichflow sensor comprises excitation means for causing the tube to oscillateabout an excitation axis as well as detection means for detectingdisplacements of portions of the tube during operation. The tubefixation means is connected to a balancing member, the assembly of thebalancing member and the tube being resiliently arranged with respect tothe housing, while the excitation means are “internal” and are connecteddirectly or indirectly to the tube fixation means. As a result, duringexcitation the tube will rotate about the excitation axis incounter-phase with the balancing member.

1. A Coriolis flow sensor, comprising: a loop shaped Coriolis tubemounted in a housing with two ends lying next to one another, the endsbeing fixed in a tube fixation means, a portion of the tube locatedbetween the ends lying free from the housing; excitation means forcausing the tube to oscillate about an excitation axis; and detectionmeans for detecting displacements of portions of the tube duringoperation, wherein the tube through the tube fixation means is connectedto a balancing member, an assembly of the balancing member and the tubebeing resiliently arranged with respect to the housing, the excitationmeans being configured to rotate the tube about the excitation axis incounter-phase with the balancing member.
 2. The Coriolis flow sensor asclaimed in claim 1, wherein the assembly of the balancing member and thetube is suspended relative to the housing by resilient means such thatthe assembly can rotate about an axis of rotation that is at leastsubstantially parallel to or coincides with the excitation axis of thetube.
 3. The Coriolis flow sensor as claimed in claim 1, wherein thetube ends merge into a feed tube and a discharge tube beyond the tubefixation means, the feed tube and the discharge tube being fixedlyconnected to a feed block and a discharge block, respectively, the feedand discharge blocks constituting the sole resilient means.
 4. ACoriolis flow sensor, comprising: a loop shaped Coriolis tube mounted ina housing with two ends lying next to one another, the ends being fixedin a tube fixation system, a portion of the tube located between theends lying free from the housing; at least one actuator configured tocause the tube to oscillate about an excitation axis; and at least onedetector configured to detect displacements of portions of the tubeduring operation, wherein the tube through the tube fixation system isconnected to a balancing member, an assembly of the balancing member andthe tube being resiliently arranged with respect to the housing, the atleast one actuator being configured to rotate the tube about theexcitation axis in counter-phase with the balancing member.
 5. TheCoriolis flow sensor as claimed in claim 4, wherein the assembly of thebalancing member and the tube is suspended relative to the housing by aresilient device such that the assembly can rotate about an axis ofrotation that is at least substantially parallel to or coincides withthe excitation axis of the tube.
 6. The Coriolis flow sensor as claimedin claim 4, wherein the tube ends merge into a feed tube and a dischargetube beyond the tube fixation system, the feed tube and the dischargetube being fixedly connected to a feed block and a discharge block,respectively, the feed and discharge blocks constituting the soleresilient device.